Gene McNeely - Experimental Aircraft Builder's Log

Neals Web Site


Date: 9-12-2005
Number of Hours: 2.00
Manual Reference:
Brief Description: Flaps

Used the 2x8 bend break to tighten the trailing edge bend in the top left skin. Clecoed the skin to the flap skeleton and match-drilled the span-wise row of rivet holes in the bottom skin.

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